- Serial number
- 7638
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Certificate issued
- March 28, 2024
- Expires
- March 31, 2031
- Mode S code
- A55767
- Registered owners
- Corporate Flight Management IncdbaContour Aviation
- Location
- Smyrna, TN
- Owner type
- Corporation
From the FAA registry file of October 20, 2026.
On this page
Airworthiness directives that may apply · 159
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment. Not a compliance determination.
| 1981 | 1 |
|---|---|
| 1982 | 6 |
| 1993 | 1 |
| 1994 | 6 |
| 1995 | 4 |
| 1996 | 2 |
| 1997 | 3 |
| 1998 | 4 |
| 1999 | 5 |
| 2000 | 5 |
| 2001 | 5 |
| 2002 | 7 |
| 2003 | 12 |
| 2004 | 10 |
| 2005 | 10 |
| 2006 | 13 |
| 2007 | 7 |
| 2008 | 17 |
| 2009 | 7 |
| 2010 | 13 |
| 2011 | 9 |
| 2012 | 6 |
| 2013 | 7 |
| 2014 | 6 |
| 2015 | 5 |
| 2016 | 7 |
| 2017 | 3 |
| 2018 | 1 |
| 2019 | 5 |
| 2020 | 9 |
| 2021 | 3 |
| 2022 | 3 |
| 2023 | 5 |
| 2024 | 3 |
| 2025 | 3 |
| 2026 | 3 |
Airframe · Bombardier CL-600-2B19
AD 2026-13-02NavigationAD 2026-05-05Flight controlsAD 2026-02-03Flight controlInformation bulletins that may apply · 9
Advisory, not mandatory. Matched the same way as ADs.
Airframe · Bombardier CL-600-2B19
SAIB NM-10-06Oxygen Inspection of Third Crewmember Oxygen HoseSAIB NM-09-03Engine Fuel and Control - Implementing Fuel Tank System Airworthiness LimitationsSAIB NM-07-26Flap failures during cold weather operationsSAIB NE-07-25Thrust reverser access cowlsSAIB NM-07-11Brake System AccumulatorsSAIB NM-05-60SAIB NM-05-55SAIB NM-05-53SAIB NM-05-31NTSB investigations
No NTSB investigations matched to N443SWMatched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Bombardier CL-600-2B19 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date.
Service difficulty reports · 151
SDR SWIA202158377Frame · corrodedMAIN AVIONICS COMPARTMENT, FRAME FS 394.00 HAS SURFACE CORROSION ON FWD LOWER CAP BETWEEN STGR 26L-26R. (FILED CLOSED) REMOVED AND REPLACED SKIN SUPPORT ON FWD SIDE OF FRAME FS394.00 IN REF TO SRM 51-42-06 AND 51-42-21. COMPLIED WITH TASK CARD 51-900-10SDR SWIA202005110570Skin · scratchedTRANSFER FROM EAML 410648 : SCRATCH DOWN TO BARE METAL. APROX 5 FEET BEHIND SERVICE DOOR, EYE LEVEL. DAMAGE FOUND TO BE AT FUSELAGE SKIN BETWEEN FS409.00 AND FS409.00+16 AND BETWEEN STR15R AND STR18R.REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN FS409.00 AND FS409.SDR SWIA2019080846171Strut · failedGEAR DISAGREE AFTER TAKEOFF. FOLLOWED QRH - RTF. FLT 4992. REMOVED AND REPLACED NLG DRESSED SHOCK STRUT IAW AMM. OPS CHECK GOOD.
See all 151 reports